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Skymark Aerospace  //  Aircraft System

Skymark
Hawk

An unmanned aerial interceptor platform combining a common airframe with configurable propulsion and a modular sensor architecture, allowing each configuration to be tailored to specific mission requirements.

Platform UAS
Status In development
Configuration Modular
Skymark Hawk // Interceptor
01  //  Platform

A Modular Interceptor Platform

Skymark Hawk combines a common airframe with interchangeable propulsion and sensor modules, allowing the platform to be configured to suit specific mission requirements.

Development is ongoing. Geometry, mass distribution and system integration are being refined across successive prototypes.

  • 01

    Configurable propulsion

    Propeller and ducted fan options are being developed for a common airframe.

  • 02

    Modular Sensing

    A common sensor bay is intended to support alternative sensor packages.

  • 03

    Common Aeroframe

    A shared airframe provides the basis for the planned configurations.

  • 04

    Mission Configuration

    Propulsion and sensor options are selected to suit mission requirements.

02  //  Configuration

Explore Configurations

Explore the propulsion and sensor options being developed for Skymark Hawk. Configurations are illustrative and may change during development.

Skymark Hawk unmanned aircraft Configuration view HWK / 01
Skymark Hawk // Flight configuration
Skymark Hawk aircraft detail Aircraft detail HWK / 02
Skymark Hawk // Platform detail
Propulsion
Sensor package

Current configuration

Propulsion
Propeller
Sensor
Dual camera
Platform
Skymark Hawk
Status
In development

Architecture
Energy system
Endurance
Payload

Illustrative prototype values — interface demonstration only

03  //  Propulsion

Two propulsion paths, one structural interface.

Skymark Hawk propeller propulsion module

Propulsion close-up — propeller  //  3:2

01

Propeller

A propeller configuration designed to prioritize endurance. Performance remains subject to validation.

Architecture
Open rotor, outboard
Design focus
Endurance
Profile
Extended loiter
02

Ducted Fan

A ducted fan configuration designed to prioritize speed. Performance remains subject to validation.

Architecture
Open rotor, outboard
Design focus
Endurance
Profile
Extended loiter
Skymark Hawk impeller propulsion module

Propulsion close-up — impeller  //  3:2

04  //  Sensing

Sensor configurations.

The sensor architecture is being developed to support alternative camera packages within a common forward bay.

01

Dual camera system

A proposed two-camera arrangement combining wide and narrow fields of view.

Channels
Two, simultaneous
Field
Wide + narrow
Mount
Shared, stabilised
02

High Magnification Camera

A proposed camera configuration for detailed observation within a narrow field of view.

Channels
One, long-range
Field
Narrow
Mount
Stabilised, single axis
05  //  Data

Engineering data.

Airframe length 65 cm
Airframe mass 5.6 kg
Energy system Electric, modular
Cruise velocity 150 km/h
Sensor interface Single forward bay
Operating envelope Under validation
Maximum span 35 cm
Propulsion architecture Configurable
Endurance Up to 2 h
Payload capacity 1 kg
Control system Assisted autonomy
Configuration type Modular

Platform specifications remain under validation and may change during development.

06  //  Detail

Take a closer look.

Skymark Hawk is being developed as a modular unmanned aircraft platform capable of supporting multiple propulsion and sensor configurations.

Status In development
Configuration Modular